JASC 5310
Service difficulty reports · 38,528
Reports filed under 5310 · Fuselage Main, Structure, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5310' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5310' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CALA2024051501482Window Frame · damagedWINDOW FRAME CENTER POST HAS OUT OF ROUND HOLES REF. HAECO LCQ S.O. 375260 NR 30866. UPDATING MAJOR REPAIR AND SDR TO YES ACCOMPLISHED REPAIR ON WINDOW FRAME CENTER POST HOLES PER HAECO REO ? L25010 REV IR AND ECRA 5311-03174 REV A WITH NO DEVIATION. REF. LP 7SDR CALA2024051401474Window Post · crackedRH #1 WINDOW FRAME RIGHT POST HAS 1 (EA) CRACK IN UPPER CORNER REF EA 5310-04554 OP 004 REV C STEP 9 (A)(B) AND PARAGON NDT NDI REPORT JOB # F060524 DATED MAY 6, 2024. TRANSFER REF NON-ROUTINE LP# 7010407. 1 EA CRACK ON RH #1 WINDOW FRAME UPPER CORNER REPAIREDSDR FDEA202405130659Crease Beam · corrodedRBL 63 STATION 860 TO 880 CREASE BEAM HAS AREAS OF CORROSION. CORROSION FOUND OUT OF LIMITS. REMOVED AND REPLACED CREASE BEAM P/N BAC 1515 553124 BATCH NUMBER 0002677936 IAW SRM 53-30-13-01 AND SRM 51-40-02. MAJOR REPAIRSDR ASAA2024051252152Beam · gougedL/H FWD OVER WING EMERGENCY EXIT DOOR, INTERNAL UPPER HORIZONTAL BEAM LOWER EDGE IS GOUGED 2EA SPOTS MARKED. GROUNDED - YES. REMOVED (4EA) CLIPS AND DAMAGED BEAM 1EA AS WELL AS INSULATION AND HANDLE ASSY. IAW AIRBUS A320-214 CMM 52-21-11-010-803-A01 & SRM 51-4SDR ASAA2024051252118Beam · gougedR/H AFT OVER WING EMERGENCY EXIT DOOR, INTERNAL UPPER HORIZONTAL BEAM LOWER EDGE IS GOUGED 2EA SPOTS MARKED GROUNDED - YES. REMOVED GOUGED BEAM & AND LOCATED, DRILLED, AND INSTALLED (1EA) SERVICEABLE BEAM, AS WELL AS REINSTALLED DISPLACED SEAL, HANDLE ASSY, PESDR ASAA2024051252117Beam · wornL/H AFT OVER WING EMERGENCY EXIT DOOR, INTERNAL UPPER HORIZONTAL BEAM LOWER EDGE IS GOUGED 2EA SPOTS MARKED GROUNDED - YES. REMOVED DAMAGED BEAM, LOCATED, DRILLED (1EA) SERVICEABLE BEAM. INSTALLED (1EA) SERVICEABLE BEAM, AND REASSEMBLED DOOR ASSY, SEAL HANDLE SDR ASAA2024051252116Beam · wornR/H FWD OVER WING EMERGENCY EXIT DOOR, INTERNAL UPPER HORIZONTAL BEAM LOWER EDGE IS GOUGED 2EA SPOTS MARKED. GROUNDED - YES. REMOVED DAMAGED BEAM, LOCATED, DRILLED (1EA) SERVICEABLE BEAM. INSTALLED, (1EA) SERVICEABLE BEAM, AND REASSEMBLED DOOR ASSY, SEAL, HANSDR AALA202405209475Splice · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPLICE INBOARD SIDE UPPER POSITION LOCATED AT Y1162 LOCATED AT LEVEL FR 68 IN AFT GALLEY AREA. REPLACED SPLICE PER SRM 51-42-11-801.SDR IPXA2024072425041Splice · crackedDAMAGE FOUND IN HOLES (A, E, L, M, AND N) CRACK/DAMAGE FOUND IN HOLE (H) ON FR47 LH SPLICE FITTING. AREAS MARKED IN RED. ACCOMPLISHED THE REPAIR PER EO-90930-REQ1 AND EA 300-5315-27-A3616 REV. -. JOB COMPLETE. REVIEWEDSDR SWAA2024061485675Panel · corrodedP15 REFUEL PANEL FACEPLATE HAS SPOTS OF CORROSION<[01] REMOVED THE REFUEL PANEL AS PER REFERENCE AMS 28-41-61-000-801; INSTALLED P15 REFUEL PANEL AS PER AMM 28-21-00-400-801; PERFORMED REFUEL PANEL INSTALLATION TEST AS PER AMM 28-21-00-400-801. TEST FOUND NORMSDR DALA2024051405192Door Frame · damaged(LOG 0340966) E&E ACCESS DOOR CUTOUT WEB HAS SCRATCH AT STA 344 O/B. REMOVED AND REPLACED DAMAGE WEB AT STA 344 O/B RIGHT SIDE PER B737-800 SRM 51-40-05-0G AND DWG 141A8511 REV.C.SDR IPXA2024062707930Structure · crackedCRACKS/DAMAGE FOUND IN ALL 3 HOLES ON FR40 RH UPPER TENSION BOLTS. TOP HOLE (3 SMALL CRACKS IN 1ST LAYER) MIDDLE HOLE (PITTED CORROSION AT START OF HOLE) BOTTOM HOLE (CRACK AT START OF HOLE). ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-90914-REQ1 AND VT-MAE EA 3SDR SWAA2024061484450Panel · corrodedREFUEL PANEL (P15) FACE PLATE HAS SIGN OF CORROSION AROUND FUEL QTY GAUGES.<[01] REMOVED REFUEL PANEL (P15) AS PER B737 AMM TASK 28-21-00-000-801.<BR>INSTALLED EWIS PROTECTION FOR MAINTENACE AS PER B737 AMM TASK 20-60-07-913-801.<BR>REPLACED FACEPLATE/BRACKET SDR R61A2024053100245Beam · corrodedCORROSION ON FWD CARGO DOOR BEAM ALONG BOTTOM EDGE OF THE CENTER SEAL DEPRESSOR FRAME BETWEEN FRAME 24 AND 26.SDR DALA2024051905327Window Frame · damagedAIRCRAFT 3703, SECTION IV HFEC INSPECTION PER ER/A 617372-14 REV A ISSUED FOR PERMANENT REPAIR OF THE #1 LH FLIGHT COMPARMENT WINDOW FRAME REPAIR. FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND TRIPLER PESDR R61A2024051600229Doubler · corrodedFUSELAGE WASTE BOX CUTOUT INTERNAL SURFACE HAS AREA OF CORROSION AT FR 88 AND STGR 26R. REMOVED AND REPLACED FUSELAGE WASTE BOX CUTOUT INTERNAL DOUBLER AT FR 88 AND STGR 26R. REF EMB SRM 51-40-08. SEE WIPS AND TASKS FOR WORK ACCOMPLISHED.SDR YENA2024051500736Beam · corrodedDURING HEAVY MAINTENANCE: CORROSION ON PREVIOUS REPAIR DOUBLER PLATE OF CENTRAL LONGITUDINAL BEAM LOCATED BTW FR84 TO FR 85 AND Y=289RH OF CABIN PAX FLOOR STRUCTURE AT CENTER FUSELAGE III W2; REF: TOMX W/O 2552 N/R 00088 REPLACED PER EMB-190 SRM 51-12-01, SRM SDR DALA2024051305132Door Frame · damagedBENT AND MISSING MATERIAL ON AFT EDGE OF FWD CARGO DOOR CUTOUT AT EXTERNAL FUSELAGE. SUMMARY OF NRC 00008: AFT EDGE OF FWD CARGO DOOR CUTOUT AT EXTERNAL FUSELAGE WAS REPAIRED PER ERA 617722-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-617722SDR AALA202409186697Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING CRACKED BETWEEN FR 1 AND FR 2 AT Y0. REPLACED CONTINUITY FITTING PER EO 5319Y017-002.SDR JJBA20240520037Crossbeam · crackedNLG W/WELL CRACK FOUND ON NLG UP-LOCK AFT CROSSBEAM. NLG WHEEL WELL AFT CROSS BEAM REMOVED AND REPLACEDSDR JJBA20240520036Crossbeam · crackedNLG W/WELL CRACK FOUND ON NLG UP-LOCK FWD CROSSBEAM. NLG WHEEL WELL FWD CROSS BEAM REMOVED AND REPLACED.SDR CALA2024051301467Window Frame · cracked(SUPPORT TASK) #1 WINDOW FRAME HAS 1 EA CRACK VERIFIED BY NDT HFEC WINDOW FRME CRACKED NON-ROUTINE IS FOR SPR REPOTABLE REPAIRED ON EA5310-04554 RV C SEQ 1008.SDR JR2R20240509231Doubler · corrodedTEXAS DOUBLER FR90 RBL24 CORRODED. REPLACEDSDR 2A6D20240509002Bonding Plate · corrodedDAMAGE IS ON THE TAIL BOOM VHF ANTENNA BASE PLATE (P/N: 350A65-1707.00) IN THE FORM OF CORROSION. THE BASE PLATE IS EXCESSIVELY CORRODED AND DEPTH OF THE DAMAGE IS ALL THE WAY THROUGH THICKNESS WHICH RESULTS IN REPLACEMENT OF ANTENNA BASE PLATE.SDR SWIA2024F00567Door Frame · corrodedPAX DOOR FRAME 313.56 HAS EXFOLIATED CORROSION JOB # HN00158803 (C-CHECK RO 7/9/2024) INSTALLED NEW PAX DOOR FRAME 313.56 REF CRJ900 SRM 51-42-06-001-001-A01, DWG 601R31702 REV -N. COMPLIED WITH M-337 AND SKYWEST TASK CARD 51-900-1002-SKY NO LEAKS NOTEDSDR AALA202406212295Fork · wornAIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU LEFT HAND LATERAL FORK END FITTING WORN ALLOWING CONTACT BETWEEN FITTING BOLT AND STRUCTURE, BETWEEN FR 23 AND FR 24 AT+Y1292, BETWEEN S32L AND S33L. REPLACED LEFT HAND LATERAL FORK END FITTING PESDR NACA2024050800001Door Frame · crackedFOUND A CRACK AT THE FORWARD SERVICE DOOR CUTOUT AFT LOWE CORNER FASTENING HOLES. THE DAMAGED AREA WAS TRIMMED OUT. REPAIR PARTS MADE AND INSTALLED IAW SRM 53-10-01-2R.SDR JJBA20240611023Beam · corrodedRF1, CARGO ENTRANCE LOWER BEAM BTW FR65-68 FOUND CORRODED. RF1, CARGO ENTRANCE LOWER BEAM BTW FR 65-68 CORROSION OUT OF LIMIT AND BEAM REMOVED AND REPLACEDSDR CALA2024050901416Door Frame · scratchedE&E COMPARTMENT DOOR CUTOUT FRAME/WEB AREAS HAVE SMALL GOUGES/SCRATCHES AND WORN , L/P CREATED FOR PURPOSE OF ESFR ONLY SEE N/R 1985479 FOR WORK PERFORMED.SDR 2A6D20240508003Crosstube · corrodedTHE AFT LANDING GEAR CROSSTUBE FITTING (PN: 350A21-0960.20) IS CORRODED IN MULTIPLE AREAS ON THE LOWER SURFACE. THE DEEPEST DAMAGE AREA WAS REPORTED TO BE 0.022” DEEP AND THE LARGEST AREA IS APPROXIMATELY 0.40” WIDE WITH VARIOUS LENGTHSSDR 2A6D20240508001Crossbeam · corrodedTHE RH X1790 CROSSBEAM (PN: 350A21-0572.20) IS CORRODED IN AN AREA WHERE IT CONTACTS THE RH Y400 BEAM (PN: 350A21-0587.20)SDR SCNA20250505156Strap · corrodedSECONDARY FINDING: WHILE REMOVING STRAP AT STA 800-847 WL 156 RH STR 25 FOUND CORROSIO N ON BOTTOM SIDE - REMOVED AND INSTALLED NEW STRAP AT STA 800-847 WL 156 RH PER SRM 51-40-02-OG-0 DWG 146A8180 ID: 0034 REV: -, DWG 146A8340, ID 0019, REV: -SDR SWAA2024061383608Pressure Deck · crackedCRACK FOUND ON HORIZONTAL PRESSURE DECK AT MID PASSENGER CABIN BS663+9.5 RBL 43 L: 0.7' MARKED<[01] APPLIED REPAIR ON HORIZONTAL PRESSURE DECK BS 663 BETWEEN RBL 30 TO RBL 60 PER SRM 53-40-51-2R-2 REPAIR 2;[02] VERIFIED RII ITEMS COMPLETESDR SWAA2024061083267Panel · debondedR/H; AFT AWE; HEADER PANEL FWD SIDE BOTTOM CLIP IS DISBONDED<[01] CORRECTTION SHOULD BE (R/H; AFT OWE; HEADER PANEL FWD SIDE BOTTOM CLIP IS DISBONED);[02] BONDED R/H AFT OVERWING EXIT FWD SIDE BOTTOM CLIP PER SOPM 20-50-12 TYPE 89 & REFERENCE BOEING DRAWING 41SDR FDEA202405070764Fitting · crackedTHE MDC DOOR ACTUATOR AFT SUPPORT FRAME WAS FOUND CRACK AFTER MDC DOOR REMOVED FABRICATED NEW SUPPORT FRAMES AND INSTALLED WITH FASTENERS I.A.W FEDEX EA: T6-5230- T0379032 P1, SEQ NO:774 TITLE: DOORS - CARGO DOOR/HYD SYS - MAIN CARGO DOOR ACTUATOR BEARISDR DALA2024051305152Window Frame · crackedL/H #1 WINDOW FRAME CRACK UPPER END BETWEEN #1 AND 2 WINDOW. REPAIRED L/H #1 WINDOW FRAME @ C-D POST PER SERVICE BULLETIN 737-53-1336 REV 1.SDR DALA2024051005094Window Frame · cracked(LOG 0334379) R/H #1 WINDOW FRAME CRACK UPPER END BETWEEN #1 AND 2 WINDOW. REPAIRED R/H #1 WINDOW FRAME @ C-D POST PER SERVICE BULLETIN 737 -53-1336 REV 1.SDR AALA202407191126Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE: CENTER FUSELAGE PRESSURE DECK MEMBRANE HAS 2 CRACKED FASTENER HOLES (L6 AND L7) AT FR 36 AND +Y1292. REPAIRED PRESSURE DECK MEMBRANE PER EA 354286SDR AALA202407026570Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE: CENTER FUSELAGE PRESSURE DECK MEMBRANE HAS CRACKED FASTENER HOLE AT FR 36 AND -Y1292 PLUS 1 INCH. MAINTENANCE REPAIRED PRESSURE DECK MEMBRANE PER EA 354286.SDR R61A2024053100242Crossbeam · corrodedCENTER CROSSFRAME 17 CORRODED AND TOOLING MARKS. PERFORMED PERMANENT CROSS FRAME REPAIR ON CENTER CROSS FRAME 17 REF EMB SRM 53-00-10/ REPAIR 03P.SDR R61A2024053100241Crossbeam · corrodedR/H CROSSFRAME 17 CORRODED AND TOOLING MARKS. . INSTALLED INNER DOUBLER REPAIR ON R/H CROSSFRAME 17, REF EMB SRM 53-00-10/R03.SDR CALA2024051301454Window Frame · crackedPER ECRA 5311-03212 PART 1.2: LH FRONT WINDSHIELD FRAME, LOWER NODE, CRACKED HOLE D WAS REPAIRED AT BFM. REPAIR IS A PERMANENT REPAIR WITH INSPECTION REQUIREMENTS.SDR JR2R20240504120Seal Rest · corrodedFWD CARGO DOOR CUT-OUT LWR SEAL RESTS CORRODED. REPLACED.SDR AALA202405295558Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SILL LOCATED AT FR 68 AND AT LEVEL STR 23 IN AFT GALLEY AREA. PERFORMED PERMANENT REPAIR ON LOWER SILL PER SRM 53-41-14-300-001.SDR DALA2024050604946Deck Plate · corrodedSHIP 6700 IN REF TO NRC 349: AFTER REMOVAL OF CORROSION ON DECK PLATE CORROSION OUT OF LIMITS WERE FOUND BETWEEN STA 1718/ RBL 13, STA 1718 / LBL2, STA 1718 / LBL 36. CORRECTIVE ACTION: SUMMARY OF NRC 00448: DECK PLATE BETWEEN STA 1718/ RBL 13, STA 1718 / LBL2SDR SWIA2024F00555Crossbeam · crackedFS280.00 CROSSBEAM, RBL12 ANGLE CRACKED, HN00157291 (C-CHECK RO 7/9/2024) REPLACED SUPPORT ANGLE AT FS 280 CROSSBEAM RBL 12 WITH NEW PN CC670-34099-2SB REF CRJ900 SRM 51-42-21-001-001-A01 AND DWG CC670-34010 REV K. COMPLIED WITH 51-900-1002-SKY.SDR SWIA20240710502Door Frame · scratchedMAIN AVIONICS COMPARTMENT DOOR FUSELAGE SURROUND INTERIOR LIP HAS SCUFF MARKS ALL THE WAY AROUND, HN00157285 (C-CHECK RO 7/9/2024) COMPLIED WITH REO 690-53-21-032 REV -- DATED 2008-03-07 FOR REPAIR OF SCUFF MARKS ALL THE WAY AROUND THE MAIN AVIONICSDR IPXA2024061378001Web · corrodedFAULT - CORROSION ON CENTER WING TANK REAR SPAR WEB NEAR JETTISON PUMP AT STA 1240 LBL 90. (REPAIR). REAPIR REPAIR I.A.W EO-90498-REQ1 REV.1 AND EI NO.F2024A57M-1260 REV.1. REVIEWEDSDR JJBA20240522045Window Frame · crackedCOCKPIT WINDSHIELD OVERHEAD PANEL FR PN 123-07751-005 FOUND CRACKED. LH COCKPIT OVERHEAD PANEL FR PN 123-07751-005 REPAIR PERFORMED.SDR JJBA20240522044Window Frame · crackedCOCKPIT ABOVE RH WINDSHIELD, HORIZONTAL RIB-OVERHEAD PANEL FOUND CRACKED. IN COCKPIT ABOVE RH WINDSHIELF HORIZONTAL RIB-OVERHEAD PANEL REPAIRED AND INSTALLED
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